View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 61721U 26145.26496100 +.00000000 +00000-0 +79005-5 0 00002
2 61721 53.1610 105.4354 0001307 95.9690 264.1459 15.30187511 09
| Epoch (UTC): | 25 May 2026 06:21:32 |
| Eccentricity: | 0.0001307 |
| inclination: | 53.1610° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 105.4354° |
| argument of perigee: | 95.9690° |
| revolutions per day: | 15.30187511 |
| mean anomaly at epoch: | 264.1459° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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